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AH 93-157 (ah93157-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: AH 93-157 (ah93157-il)
Reynolds number: 200,000
Max Cl/Cd: 66.24 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah93157-il-200000-n5.txt
Download as CSV file: xf-ah93157-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 93-157                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.2177   0.08988   0.08550  -0.1013   0.8461   0.0218
 -11.750  -0.2320   0.08310   0.07875  -0.1044   0.8421   0.0217
 -11.500  -0.4281   0.04615   0.04128  -0.1230   0.8346   0.0200
 -11.250  -0.4447   0.04334   0.03825  -0.1212   0.8303   0.0201
 -11.000  -0.4583   0.04097   0.03570  -0.1185   0.8254   0.0203
 -10.750  -0.4727   0.03857   0.03305  -0.1149   0.8207   0.0204
 -10.500  -0.4815   0.03678   0.03102  -0.1110   0.8169   0.0207
 -10.250  -0.4864   0.03498   0.02896  -0.1075   0.8132   0.0210
 -10.000  -0.4856   0.03311   0.02682  -0.1045   0.8095   0.0214
  -9.750  -0.4808   0.03129   0.02470  -0.1020   0.8062   0.0219
  -9.500  -0.4723   0.02953   0.02259  -0.0997   0.8032   0.0226
  -9.250  -0.4607   0.02788   0.02051  -0.0977   0.8005   0.0234
  -9.000  -0.4446   0.02680   0.01932  -0.0964   0.7976   0.0241
  -8.750  -0.4266   0.02607   0.01852  -0.0953   0.7945   0.0248
  -8.500  -0.4078   0.02534   0.01768  -0.0943   0.7916   0.0258
  -8.250  -0.3878   0.02435   0.01650  -0.0933   0.7889   0.0266
  -8.000  -0.3666   0.02334   0.01526  -0.0925   0.7864   0.0277
  -7.750  -0.3441   0.02245   0.01414  -0.0917   0.7842   0.0286
  -7.500  -0.3231   0.02174   0.01344  -0.0910   0.7815   0.0298
  -7.250  -0.3015   0.02126   0.01294  -0.0903   0.7785   0.0314
  -7.000  -0.2790   0.02067   0.01225  -0.0896   0.7756   0.0330
  -6.750  -0.2557   0.02007   0.01150  -0.0889   0.7729   0.0347
  -6.500  -0.2335   0.01941   0.01082  -0.0882   0.7706   0.0362
  -6.250  -0.2101   0.01899   0.01036  -0.0877   0.7686   0.0385
  -6.000  -0.1871   0.01860   0.00988  -0.0870   0.7660   0.0412
  -5.750  -0.1659   0.01812   0.00941  -0.0861   0.7628   0.0438
  -5.500  -0.1434   0.01775   0.00903  -0.0853   0.7598   0.0468
  -5.250  -0.1198   0.01744   0.00864  -0.0847   0.7572   0.0508
  -5.000  -0.0970   0.01703   0.00824  -0.0840   0.7547   0.0555
  -4.750  -0.0725   0.01673   0.00786  -0.0836   0.7526   0.0611
  -4.500  -0.0500   0.01641   0.00758  -0.0828   0.7500   0.0684
  -4.250  -0.0280   0.01617   0.00736  -0.0820   0.7467   0.0770
  -4.000  -0.0050   0.01592   0.00713  -0.0813   0.7435   0.0889
  -3.750   0.0184   0.01563   0.00690  -0.0807   0.7408   0.1055
  -3.500   0.0423   0.01533   0.00666  -0.0801   0.7384   0.1297
  -3.250   0.0662   0.01499   0.00642  -0.0796   0.7363   0.1647
  -3.000   0.0866   0.01469   0.00633  -0.0786   0.7330   0.2142
  -2.750   0.1055   0.01429   0.00625  -0.0773   0.7295   0.2893
  -2.500   0.1233   0.01376   0.00611  -0.0759   0.7263   0.3908
  -2.000   0.1613   0.01304   0.00687  -0.0707   0.7215   0.7521
  -1.750   0.1867   0.01344   0.00724  -0.0694   0.7189   0.8004
  -1.500   0.2042   0.01369   0.00747  -0.0673   0.7145   0.8257
  -1.250   0.2244   0.01391   0.00761  -0.0656   0.7110   0.8445
  -1.000   0.2481   0.01415   0.00776  -0.0644   0.7081   0.8584
  -0.750   0.2760   0.01439   0.00793  -0.0637   0.7058   0.8696
  -0.500   0.3006   0.01469   0.00819  -0.0624   0.7027   0.8834
  -0.250   0.3259   0.01501   0.00850  -0.0612   0.6985   0.8979
   0.000   0.3584   0.01516   0.00862  -0.0617   0.6951   0.9091
   0.250   0.3806   0.01515   0.00854  -0.0604   0.6920   0.9180
   0.500   0.4147   0.01505   0.00835  -0.0618   0.6896   0.9198
   0.750   0.4390   0.01507   0.00838  -0.0614   0.6848   0.9223
   1.000   0.4633   0.01503   0.00831  -0.0609   0.6804   0.9250
   1.250   0.4864   0.01492   0.00815  -0.0602   0.6769   0.9281
   1.500   0.5059   0.01479   0.00795  -0.0586   0.6740   0.9316
   1.750   0.5285   0.01482   0.00802  -0.0580   0.6683   0.9335
   2.000   0.5555   0.01477   0.00795  -0.0580   0.6637   0.9353
   2.250   0.5836   0.01465   0.00779  -0.0582   0.6601   0.9369
   2.500   0.6046   0.01464   0.00779  -0.0572   0.6550   0.9394
   2.750   0.6218   0.01461   0.00777  -0.0554   0.6495   0.9426
   3.000   0.6420   0.01450   0.00763  -0.0540   0.6453   0.9450
   3.250   0.6682   0.01449   0.00764  -0.0540   0.6399   0.9465
   3.500   0.6927   0.01449   0.00766  -0.0536   0.6338   0.9482
   3.750   0.7209   0.01440   0.00753  -0.0539   0.6291   0.9494
   4.000   0.7397   0.01445   0.00763  -0.0525   0.6223   0.9516
   4.250   0.7626   0.01442   0.00761  -0.0518   0.6163   0.9538
   4.500   0.7825   0.01440   0.00760  -0.0505   0.6104   0.9562
   4.750   0.8000   0.01442   0.00765  -0.0488   0.6031   0.9583
   5.000   0.8281   0.01439   0.00762  -0.0491   0.5970   0.9593
   5.250   0.8506   0.01449   0.00778  -0.0486   0.5886   0.9612
   5.500   0.8771   0.01451   0.00779  -0.0486   0.5814   0.9627
   5.750   0.8970   0.01461   0.00794  -0.0475   0.5723   0.9647
   6.000   0.9185   0.01467   0.00802  -0.0467   0.5640   0.9665
   6.250   0.9381   0.01476   0.00813  -0.0455   0.5551   0.9687
   6.500   0.9570   0.01490   0.00830  -0.0442   0.5455   0.9712
   6.750   0.9829   0.01505   0.00846  -0.0444   0.5361   0.9728
   7.000   1.0040   0.01527   0.00872  -0.0437   0.5251   0.9748
   7.250   1.0246   0.01551   0.00900  -0.0430   0.5139   0.9770
   7.500   1.0452   0.01578   0.00928  -0.0423   0.5022   0.9793
   7.750   1.0652   0.01608   0.00959  -0.0416   0.4901   0.9818
   8.000   1.0858   0.01647   0.01001  -0.0412   0.4771   0.9845
   8.250   1.1059   0.01691   0.01048  -0.0408   0.4637   0.9885
   8.500   1.1220   0.01741   0.01100  -0.0398   0.4495   0.9967
   8.750   1.1276   0.01794   0.01152  -0.0368   0.4364   1.0000
   9.000   1.1312   0.01850   0.01207  -0.0335   0.4234   1.0000
   9.250   1.1379   0.01915   0.01270  -0.0309   0.4102   1.0000
   9.500   1.1448   0.01990   0.01343  -0.0285   0.3954   1.0000
   9.750   1.1496   0.02083   0.01433  -0.0260   0.3772   1.0000
  10.000   1.1520   0.02196   0.01538  -0.0235   0.3559   1.0000
  10.250   1.1539   0.02320   0.01653  -0.0210   0.3346   1.0000
  10.500   1.1572   0.02448   0.01775  -0.0189   0.3134   1.0000
  10.750   1.1611   0.02579   0.01900  -0.0170   0.2946   1.0000
  11.000   1.1649   0.02716   0.02032  -0.0152   0.2767   1.0000
  11.250   1.1684   0.02862   0.02175  -0.0134   0.2574   1.0000
  11.500   1.1708   0.03022   0.02328  -0.0117   0.2369   1.0000
  11.750   1.1719   0.03198   0.02497  -0.0100   0.2167   1.0000
  12.000   1.1743   0.03373   0.02667  -0.0086   0.1971   1.0000
  12.250   1.1736   0.03580   0.02864  -0.0071   0.1742   1.0000
  12.500   1.1740   0.03788   0.03064  -0.0058   0.1538   1.0000
  12.750   1.1719   0.04024   0.03289  -0.0045   0.1314   1.0000
  13.000   1.1709   0.04260   0.03518  -0.0034   0.1110   1.0000
  13.500   1.1679   0.04767   0.04010  -0.0016   0.0757   1.0000
  13.750   1.1668   0.05030   0.04267  -0.0009   0.0626   1.0000
  14.000   1.1667   0.05292   0.04528  -0.0004   0.0527   1.0000
  14.250   1.1670   0.05558   0.04795   0.0000   0.0457   1.0000
  14.500   1.1673   0.05829   0.05069   0.0003   0.0404   1.0000
  14.750   1.1687   0.06098   0.05344   0.0004   0.0363   1.0000
  15.000   1.1682   0.06395   0.05647   0.0005   0.0332   1.0000
  15.250   1.1689   0.06685   0.05946   0.0004   0.0307   1.0000
  15.500   1.1693   0.06985   0.06256   0.0002   0.0283   1.0000
  15.750   1.1664   0.07331   0.06607  -0.0001   0.0264   1.0000
  16.000   1.1669   0.07645   0.06932  -0.0005   0.0249   1.0000
  16.250   1.1665   0.07974   0.07272  -0.0010   0.0237   1.0000
  16.500   1.1650   0.08324   0.07631  -0.0017   0.0225   1.0000
  16.750   1.1604   0.08722   0.08036  -0.0026   0.0215   1.0000
  17.000   1.1595   0.09074   0.08399  -0.0034   0.0206   1.0000
  17.250   1.1587   0.09433   0.08771  -0.0044   0.0196   1.0000
  17.500   1.1578   0.09796   0.09144  -0.0054   0.0187   1.0000
  17.750   1.1559   0.10179   0.09536  -0.0067   0.0180   1.0000
  18.000   1.1529   0.10579   0.09944  -0.0080   0.0175   1.0000
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